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Rapid pressure reduction test device and method for large-size aircraft assembly

A test device and aircraft technology, applied in the testing of machine/structural components, pump devices, measuring devices, etc., can solve problems such as unavailability of large-sized aircraft components, rapid decompression tests, etc., to improve rapid descent and speed up flow speed , Good universality effect

Pending Publication Date: 2020-07-31
XI'AN INST OF OPTICS & FINE MECHANICS - CHINESE ACAD OF SCI
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0012] In order to solve the technical problem that large-scale aircraft components cannot be used for rapid decompression tests using existing solutions, the present invention provides a large-scale aircraft component rapid decompression test device and method

Method used

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  • Rapid pressure reduction test device and method for large-size aircraft assembly
  • Rapid pressure reduction test device and method for large-size aircraft assembly
  • Rapid pressure reduction test device and method for large-size aircraft assembly

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Embodiment Construction

[0040] The present invention will be further described below in conjunction with accompanying drawing.

[0041] Such as figure 1As shown, the large-scale aircraft component rapid decompression test device provided by the embodiment of the present invention includes a rapid decompression tank system and an auxiliary decompression tank system.

[0042] The rapid decompression box system includes a rapid decompression box 6, a first vacuum absolute pressure transmitter 7 and a first full-scale vacuum gauge 8 arranged on the fast decompression box 6, and connected in turn to the rapid decompression box 6. The second vacuum valve 4 of an output end, the first molecular pump 3, the first vacuum valve 2 and the first mechanical vacuum pump 1; connected to the other output.

[0043] The auxiliary decompression box system includes an auxiliary decompression box 12, a second vacuum absolute pressure transmitter 13 and a second full-scale vacuum gauge 14 arranged on the auxiliary decom...

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Abstract

In order to solve the technical problem that a large-size aircraft assembly cannot be subjected to a rapid pressure reduction test by using an existing scheme, the invention provides a rapid pressurereduction test device and method for the large-size aircraft assembly. A rapid pressure reduction box is connected with a rapid pressure reduction box air exhaust unit, and the rapid pressure reduction box air exhaust unit can be used for reducing pressure simultaneously in the rapid pressure reduction process so as to increase the pressure reduction rate. Therefore, the rapid pressure reduction box is not limited by the maximum volume value and can be manufactured to be large, and then rapid pressure reduction can be conducted on the large-size aircraft assembly.

Description

technical field [0001] The invention relates to a rapid decompression test device and method, in particular to a test device and method capable of rapid decompression of large-sized aircraft components. Background technique [0002] Rapid decompression refers to the sudden loss of airtightness of the sealed cabin at high altitude, the pressure inside and outside the sealed cabin is quickly balanced, and the air pressure in the cabin suddenly drops, resulting in the impact of air waves. Its main hazards are: high altitude hypoxia, low temperature and low pressure. According to relevant data, in recent years, due to the loss of pressure in the cabin, many civil aviation airliners have frequently returned, made emergency landings or even crashed, resulting in immeasurable losses of personnel and property. The rapid decompression test is applicable to determine whether the rapid decompression of the surrounding environment pressure of the equipment will cause the equipment to r...

Claims

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Application Information

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IPC IPC(8): G01M13/00F04D19/04F04D25/16B64F5/60
CPCG01M13/00F04D19/042F04D25/16B64F5/60
Inventor 王亚军赛建刚赵燕高斌高博张海民韩磊于攀龙孟宁飞
Owner XI'AN INST OF OPTICS & FINE MECHANICS - CHINESE ACAD OF SCI
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